cornemo
Mechanical
- Apr 23, 2009
- 55
Dear all,
I'm doing a calculation for a modified flange according to ASME VIII div 2 at 310 bar and 300 degr. C (with PVElite for those that are interested). The bolt material used is the European 34CrNiMo6 (acc. EN-10269).
What I've done is the following.
- I've modelled the flange as in the design drawing.
- Then I made a max. allowables table for the material myself as the program doesn't recognize this material as allowable in an ASME calculation.
- My first problem is that no properties at high temperature are given for this material in EN-10269. I've now taken the values from PVElite EN-13445 calculation tables.
- Secondly I checked the flange and it had not enough bolt area.
- My client said to use 50% of Syt as allowable for the bolts. I however can't find a reference for this in ASME VIII nor in ASME II. I know there is appendix S which refers to higher bolt stresses during assembly. But if I make a design calculation bolt stresses should be below allowable I think.
So 2 actual questions:
- Where can I find the allowables, Yield at temperature values for 34CrNiMo6 in EN-codes for bolting materials?
- Where can I find that during an ASME flange design the bolt stress may reach to 50% of Syt?
Thanks in advance for your replies.
With regards,
Corné
I'm doing a calculation for a modified flange according to ASME VIII div 2 at 310 bar and 300 degr. C (with PVElite for those that are interested). The bolt material used is the European 34CrNiMo6 (acc. EN-10269).
What I've done is the following.
- I've modelled the flange as in the design drawing.
- Then I made a max. allowables table for the material myself as the program doesn't recognize this material as allowable in an ASME calculation.
- My first problem is that no properties at high temperature are given for this material in EN-10269. I've now taken the values from PVElite EN-13445 calculation tables.
- Secondly I checked the flange and it had not enough bolt area.
- My client said to use 50% of Syt as allowable for the bolts. I however can't find a reference for this in ASME VIII nor in ASME II. I know there is appendix S which refers to higher bolt stresses during assembly. But if I make a design calculation bolt stresses should be below allowable I think.
So 2 actual questions:
- Where can I find the allowables, Yield at temperature values for 34CrNiMo6 in EN-codes for bolting materials?
- Where can I find that during an ASME flange design the bolt stress may reach to 50% of Syt?
Thanks in advance for your replies.
With regards,
Corné